Hypersonic Flow and Heat Transfer Characteristics over an Airfoil
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Publisher
Begellhouse
Reference11 articles.
1. Tong, F., Duan, J., Jiang LAI, Sun, D., Yuan, X., Hypersonic shock wave andturbulent boundary layer interaction in asharp cone/flare model, in Chinese Journalof Aeronautics. 2022.
2. Green, J.E., Interactions between shockwaves and turbulent boundary layers.Progress in Aerospace Sciences, 1970. 11: p. 235-340.
3. Dolling, D.S., Fifty Years of Shock-Wave/Boundary-Layer Interaction Research:What Next? AIAA Journal, 2001. 39(8): p.1517-1531.
4. Jiezhi Wu, L.L., Tianshu Liu, Fundamentaltheories of aerodynamic force in viscous andcompressible complex flows. Progress in Aerospace Sciences, 2018. 99: p. 27-63.
5. Yang, Z., Wang, S., Gao, Z., Studies oneffects of wall temperature variation onheat transfer in hypersonic laminarboundary layer. International Journal of Heat and Mass Transfer, 2022. 190: p.122790.
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